Amanote Research

Amanote Research

    RegisterSign In

Aerodynamic Load of an Aircraft With a Highly Elastic Wing

Acta Polytechnica - Czech Republic
doi 10.14311/ap.2017.57.0272
Full Text
Open PDF
Abstract

Available in full text

Categories
Engineering
Date

September 1, 2017

Authors
Pavel Schoř
Publisher

Czech Technical University in Prague - Central Library


Related search

Aerodynamic Design Optimization Studies of a Blended-Wing-Body Aircraft

Journal of Aircraft
Aerospace Engineering
2014English

RANS-based Aerodynamic Shape Optimization of a Blended-Wing-Body Aircraft

2013English

Special Characteristics of Aerodynamic Properties of Unmanned Aircraft With the High-Aspect-Ratio Wing

Civil Aviation High TECHNOLOGIES
2018English

Adaptive Maneuver Load Alleviation for Flexible Wing Aircraft With Nonminimum Phase Zeros

2018English

The Effects of a Full-Aircraft Aerodynamic Model on the Design of a Tailored Composite Wing

CEAS Aeronautical Journal
TransportationAerospace Engineering
2019English

Optimization of the Aerodynamic Performance of Regional and Wide-Body-Class Blended Wing-Body Aircraft

2015English

Effect of Aerodynamic Configuration Parameters on Lateral-Directional Stability of Double-Swept Flying Wing Aircraft

Journal of Aerospace Technology and Management
Aerospace Engineering
2019English

Low Speed Aerodynamic Characteristics of an A-4 Aircraft With an Air Cushion Landing System

1973English

A New Propelled Wing Aircraft Configuration

2016English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy